Using swirl atomizer designed by this paper , kerosene was injected into the ejector combustor , and achieved steady combustion . this made a solid foundation for the future study on combustion organization 設計了旋流式霧化噴嘴,實現了煤油在引射火箭模態中的穩定燃燒,為進一步的燃燒組織研究奠定了基礎。